Joint for tiltrotor hubs

A joint is configured for use with a rotary-wing aircraft having at least one engine. A driver is coupled to an output shaft of the engine, the driver being rotatable about an axis. A yoke is at least partially rotatable relative to the driver about a first center of rotation, the center of rotation...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Stamps, Frank B, Braswell, Jr, James L, Baskin, Charles L, Zierer, Joe J, Haynie, David A, Rauber, Richard E, Campbell, Thomas C, Tisdale, Patrick R
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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